Space Charge Efgect Simulation with Liquid Argon Flow
Michael Mooney
Colorado State University
ProtoDUNE Sim/Reco Meeting June 13th, 2018
Space Charge Efgect Simulation with Liquid Argon Flow Michael - - PowerPoint PPT Presentation
Space Charge Efgect Simulation with Liquid Argon Flow Michael Mooney Colorado State University ProtoDUNE Sim/Reco Meeting June 13 th , 2018 Introduction Introduction Expect space charge efgects (SCE) to be one of two leading detector
Michael Mooney
Colorado State University
ProtoDUNE Sim/Reco Meeting June 13th, 2018
♦ Expect space charge efgects (SCE) to be one of two leading detector efgects at ProtoDUNE-SP
♦ Open question: how much do we expect fmow of liquid argon to impact underlying space charge confjguration?
argon fmow velocity are similar in magnitude
detector, or at least modify space charge distribution
♦ Today: show fjrst study of LAr fmow on SCE
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♦ Developed by Erik Voirin for ProtoDUNE-SP (previously produced for 35-ton) – see DUNE Doc DB #928 ♦ 3D simulation of LAr fmow, 8 mm/s ion drift @ 500 V/cm, uniform space charge deposition from cosmics ♦ Ion absorption at fjeld cage, APA, CPA, and all solid
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♦ Make use of code suite developed by M. Mooney for simulation of SCE given space charge density map from Erik’s simulation
♦ Fourier series solution for electric fjeld on grid, radial basis functions for interpolation of fjeld between grid points, and ray tracing based on RK45 for determining spatial displacements due to SCE ♦ Nominally assumes linear space charge distribution (zero at anodes, maximal at cathode), but code suite has capability of using arbitrary space charge distribution as input
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♦ Transverse spatial distortions (TPC top/bottom)
distortions at TPC top (see later slides!)
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♦ Main efgects of liquid argon fmow on SCE:
nominal case (no fmow)
– Ion deposition rate used by M. Mooney and Erik are almost identical: ~2×10-10 C/m3/s
♦ Distributions still smoothly vary across drift volumes, as in nominal case ♦ Noteworthy: no large build-up of space charge predicted in any one place when including efgects of fmuid fmow ♦ Useful case study for qualitative understanding, but may be very difgerent in reality
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Half Field Vs. No Flow: Z = 3.6 m Half Field Vs. No Flow: Z = 3.6 m
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♦ Space charge efgects: build-up of slow-moving argon ions in TPC volume due to large cosmic fmux (affmicting near-surface LArTPCs, e.g. ProtoDUNEs)
distortions in position of reconstructed ionization charge
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DUNE SP Far Detector DUNE DP Far Detector ProtoDUNE DP ProtoDUNE SP
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250 V/cm 500 V/cm
~20 cm spatial distortions ~60 cm spatial distortions
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♦ Muon halo can fjll in gap (active volume in red, above) ♦ However, relative to cosmics, rate is low: O(100)/spill ♦ Need CRT triggers to save as many as possible
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Muon Halo Coverage Map (ProtoDUNE-SP TDR) units: μ/m2/spill (spill length: 4.8 s)
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0-tagging Methods
♦ What about using other t0-tagging methods to fjll gaps? ♦ For example, MicroBooNE’s anode/cathode piercers:
♦ But this sample still sees a gap in the middle of TPC...
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Anode- Piercers Cathode- Piercers